Encyclopedia Astronautica
November 29


November 29 Chronology


1908 November 29 - .
  • Birth of Kurt Heinrich Debus - . Nation: Germany; USA. Summary: German-American engineer. At Peenemuende from 1940, designed and operated V-2 test launch facility. In US from 1945, headed design, build, and operation of launch facilities for the V-2, Redstone, Jupiter, and Saturn rockets for Apollo..

1944 November 29 - . Launch Site: Heidekraut. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 19825.
  • V-2 Ma277 271 P14 - . Nation: Germany. Summary: Planned range 225 km. Impact 10.7 km to the left of the planned trajectory. Circular error 12.3 km from aim point..

1946 November 29 - . Launch Vehicle: Keldysh Bomber.
  • Keldysh Space Bomber authorised - . Nation: USSR. Related Persons: Keldysh; Saenger. Program: Navaho. The NII-1 NKAP research institute was formed with Mstislav Vsevolodovich Keldysh as its head to investigate and develop the German Saenger-Bredt design. It was clear from the preliminary study that an immense amount of work needed to be done before a draft project of a feasible design could be prepared - it would take until the mid-1950's.

1948 November 29 - .
  • XS-1 Flight 98 - . Crew: Champine. Payload: XS-1 # 2 flight 41. Nation: USA. Related Persons: Champine. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: NACA flight 21. Check on handling qualities and pressure distribution. Mach 0.88..

1949 November 29 - .
  • Birth of Kenneth Donald Cameron - . Nation: USA. Summary: American test pilot astronaut. Flew on STS-37, STS-56, STS-74. US Marine Corps.

1949 November 29 - .
  • XS-1 Flight 128 - . Crew: Everest. Payload: XS-1 # 1 flight 75. Nation: USA. Related Persons: Everest. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: AF flight 53. High-altitude wing-tail loads investigation..

1951 November 29 - . Launch Site: Holloman. Launch Complex: Holloman SLED. LV Family: Snark. Launch Vehicle: MX-775.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 10 km (6 mi).

1954 November 29 - . Launch Site: White Sands. LV Family: Honest John. Launch Vehicle: Honest John. LV Configuration: Honest John 449ES.
  • Test mission - . Nation: USA. Apogee: 10 km (6 mi).

1955 November 29 - .
1955 November 29 - . 17:16 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-N-10. LV Configuration: Aerobee RTV-N-10 NRL 24.
  • Mass spectrometers Ionosphere mission - . Nation: USA. Agency: NRL. Apogee: 132 km (82 mi). Summary: Ion composition research. Launched at 1016 local time. Reached 132 km..

1956 November 29 - . 13:23 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC6. LV Family: Redstone. Launch Vehicle: Jupiter A. LV Configuration: Jupiter A CC-15.
  • Jupiter A - . Nation: USA. Agency: USA. Apogee: 90 km (55 mi). Launched at 0823 hours EST from AMR. The flight was successful. Actual range was 138.969 nm; .137 nm over and 122 meters left of the intended impact point, a radial miss distance of 260 meters. The primary test objectives were to test the accuracy of the complete guidance system and to test Jupiter control components. Missed aimpoint by 255 m.

1958 November 29 - . 02:27 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC14. LV Family: Atlas. Launch Vehicle: Atlas B. LV Configuration: Atlas B 12B.
  • Research and development / AFSWC-3 test - . Nation: USA. Agency: USAF. Apogee: 900 km (550 mi). Summary: Less than 18 months after the first flight, a USAF Atlas made its first successful full-range operational test flight in a 6,325 statute-mile flight, landed close to its target..

1958 November 29 - . 16:30 GMT - . Launch Site: Fort Churchill. LV Family: Aerobee. Launch Vehicle: Aerobee Hi. LV Configuration: Aerobee Hi NN3.16F.
  • Auroral / Ultraviolet Phot Aurora mission - . Nation: USA. Agency: NRL. Apogee: 202 km (125 mi).

1960 November 29 - .
  • Briefing on the Apollo and Saturn programs - . Nation: USA. Related Persons: von Braun; Faget. Program: Apollo. Spacecraft: Apollo CSM; CSM Source Selection; LM Mode Debate; LM Source Selection. A joint briefing on the Apollo and Saturn programs was held at Marshall Space Flight Center MSFC, attended by representatives of STG and MSFC. Maxime A. Faget of STG and MSFC Director Wernher von Braun agreed that a joint STG-MSFC program would be developed to accomplish a manned lunar landing. Areas of responsibility were: MSFC launch vehicle and landing on the moon; STG - lunar orbit, landing, and return to earth.

1960 November 29 - . 11:16 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NB3.103.
  • NRL NB3.103 Ultraviolet astronomy mission - . Nation: USA. Agency: NRL. Apogee: 197 km (122 mi).

1961 November 29 - .
  • Glenn selected for the first Mercury manned orbital flight. - . Nation: USA. Related Persons: Glenn; Carpenter. Program: Mercury. Astronaut John Glenn was selected as the pilot for the first Mercury manned orbital flight, with Scott Carpenter as backup pilot. Immediately, training was started to ready these two astronauts for the mission. The five remaining astronauts concentrated their efforts on various engineering and operational groups of the Manned Spacecraft Center in preparation for the mission.

1961 November 29 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC19. LV Family: Titan. Launch Vehicle: Titan 1. LV Configuration: Titan I M-5.
  • Mk 4 re-entry vehicle test - . Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi).

1961 November 29 - . Launch Site: Baikonur. Launch Complex: Baikonur LC41/4. Launch Pad: LC41?/pad?. LV Family: R-16. Launch Vehicle: R-16.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).

1961 November 29 - . 15:07 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC14. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 93D.
  • Mercury MA-5 - . Payload: Mercury SC9. Mass: 1,300 kg (2,800 lb). Nation: USA. Agency: NASA. Program: Mercury. Class: Manned. Type: Manned spacecraft. Spacecraft: Mercury. Decay Date: 1961-11-29 . USAF Sat Cat: 208 . COSPAR: 1961-A-Iota-1. Apogee: 237 km (147 mi). Perigee: 158 km (98 mi). Inclination: 32.6000 deg. Period: 88.30 min. Mercury-Atlas 5 (MA-5), the second and final orbital qualification of the spacecraft prior to manned flight was launched from Cape Canaveral with Enos, a 37.5 pound chimpanzee, aboard. Scheduled for three orbits, the spacecraft was returned to earth after two orbits due to the failure of a roll reaction jet and to the overheating of an inverter in the electrical system. Both of these difficulties could have been corrected had an astronaut been aboard. The spacecraft was recovered 255 miles southeast of Bermuda by the USS Stormes. During the flight, the chimpanzee performed psychomotor duties and upon recovery was found to be in excellent physical condition. The flight was termed highly successful and the Mercury spacecraft well qualified to support manned orbital flight.

1961 November 29 - . 23:01 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B2. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 53D.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi).

1962 November 29 - .
  • Final tests for female cosmonauts. - . Nation: USSR. Program: Vostok. Flight: Vostok 5; Vostok 6; Vostok 6A. Academic examinations were completed of the female cosmonaut corps. Kuznetsova had missed to much training and was excluded from even taking the test. Of the four women remaining, only Tereshkova did not receive the highest marks. This was attributed to her being too nervous and excited during the examination. All were given the rank of Junior Lieutenant in the VVS Soviet Air Force.

    Kamanin considered Tereshkova as the leading candidate for the first flight, with Solovyova as her back-up. In personality they were equivalent to Gagarin/Nikolayev - indeed, Tereshkova was considered 'Gagarin in a skirt'. Ponomaryova and Yerkina were equal candidates for the second female Vostok flight. The group would go to a resort in the Urals from 30 November to 10 January. The final decision as to which one would fly would only be made 3 or 4 days before the flight.


1962 November 29 - . Launch Site: White Sands. Launch Complex: White Sands LC38. LV Family: Nike Zeus. Launch Vehicle: Nike Zeus. LV Configuration: Nike Zeus-3.
  • Simulated target - . Nation: USA. Agency: USA. Apogee: 200 km (120 mi).

1962 November 29 - . 16:33 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA5B. Launch Pad: LA5B?. LV Family: Black Knight. Launch Vehicle: Black Knight 301/C. LV Configuration: Black Knight-301/C BK.18.
  • Gaslight Re-entry Vehicle test - . Nation: UK. Agency: RAE. Apogee: 576 km (357 mi).

1963 November 29 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1A. LV Configuration: Minuteman 1A 642.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1965 November 29 - . Launch Site: San Nicolas. LV Family: Redstone. Launch Vehicle: Redstone.
  • Project Defender Redstone launch. - . Nation: USA. Summary: Redstone launched as ballistic missile target and was successfully intercepted by a US Navy Terrier surface-to-air missile launched from Point Mugu, California..

1965 November 29 - . 04:48 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2E. LV Family: Delta. Launch Vehicle: Thor Agena B SLV-2. LV Configuration: Thor SLV-2 Agena B 453 (TA5) / Agena B S-01 6102 .
  • Alouette 2 - . Payload: Alouette 2 / Explorer 31. Mass: 145 kg (319 lb). Nation: Canada. Agency: DRTE. Class: Earth. Type: Magnetosphere satellite. Spacecraft: Alouette. USAF Sat Cat: 1804 . COSPAR: 1965-098A. Apogee: 2,666 km (1,656 mi). Perigee: 503 km (312 mi). Inclination: 79.8000 deg. Period: 117.90 min. Ionospheric research; data correlated with Explorer 31. The double-launch project, known as ISIS-X was the first in a new co-operative NASA-Canadian Defense Research Board program for International Satellites for Ionospheric Studies. Alouette was in orbit with an apogee just over a kilometre lower than Explorer 31's and with a perigee of just more than a kilometre higher. The orbits were some 3000 km at apogee and 500 km at perigee.
  • Explorer 31 - . Payload: DME A. Mass: 99 kg (218 lb). Nation: USA. Agency: NASA Greenbelt. Program: Explorer. Class: Earth. Type: Ionosphere satellite. Spacecraft: DME. USAF Sat Cat: 1806 . COSPAR: 1965-098B. Apogee: 2,833 km (1,760 mi). Perigee: 505 km (313 mi). Inclination: 79.8000 deg. Period: 119.70 min. Ionospheric research; data correlated with Alouette 2. The Explorer 31, Direct Measurement Explorer, was launched with a Canadian Alouette II on November 28, 1965, on a Thor-Agena rocket from Vandenberg Air Force Base, California. The double-launch project, known as ISIS-X was the first in a new co-operative NASA-Canadian Defense Research Board program for International Satellites for Ionospheric Studies. Explorer 31 was in orbit with an apogee just over a kilometre more than Alouette's and with a perigee of just more than a kilometre lower. The orbits were some 3000 km at apogee and 500 km at perigee. Eight ionospheric measurement experiments sampled the environment both forward and after the satellite's path.

1965 November 29 - . 14:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 200D.
  • NTMP KX-33 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1966 November 29 - . 01:06 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna C. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure CE-8.
  • ESRO C9 / 2 Aurora mission - . Nation: Europe. Agency: ESRO. Apogee: 149 km (92 mi).

1966 November 29 - . 06:01 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 3. LV Configuration: Black Brant III AAF-3-12.
  • Plasma / fields mission - . Nation: Canada. Agency: NRCC. Apogee: 114 km (70 mi).

1966 November 29 - . 06:08 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 4A. LV Configuration: Black Brant IVA AAF-4-05.
  • CR / ne probe Plasma / fields mission - . Nation: Canada. Agency: NRCC. Apogee: 800 km (490 mi).

1966 November 29 - . 19:38 GMT - . Launch Site: Hidden Hills DZ. Launch Pad: 36.1 N x 116.0 W. Launch Platform: NB-52 003. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 3-57-86.
  • X-15A Checkout mission - . Nation: USA. Agency: NASA; USAF. Apogee: 28 km (17 mi). Summary: Maximum Speed - 5020 kph. Maximum Altitude - 28040 m..

1967 November 29 - .
  • Kamanin appeals for 7K-VI program to continue. - . Nation: USSR. Spacecraft: Soyuz VI. Kamanin writes a letter to the Central Committee on the need for the 7K-VI spacecraft for military research. He also complains about his problems in obtaining adequate spacecraft simulators. Later he meets with Grigoriy Nikolayevich Postukov, sculptor of cosmonaut statutes.

1967 November 29 - . 01:06 GMT - . Launch Site: Sonmiani. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.250IM.
  • Rehbar 14 (Grenades) Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 175 km (108 mi).

1967 November 29 - . 04:49 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA8. LV Family: Redstone. Launch Vehicle: Sparta. LV Configuration: SPARTA 2029/SV-10.
  • Wresat 1 - . Payload: Wresat / BE-3. Mass: 45 kg (99 lb). Nation: Australia. Agency: WRE. Class: Earth. Type: Atmosphere satellite. Spacecraft: Wresat. Decay Date: 1968-01-10 . USAF Sat Cat: 3054 . COSPAR: 1967-118A. Apogee: 1,252 km (777 mi). Perigee: 198 km (123 mi). Inclination: 83.3000 deg. Period: 99.30 min. Summary: Weapons Research Establishment Satellite; solar radiation, upper atmosphere data. WRESAT 1 launched for upper atmosphere and space research at 1419 h central standard time, from Woomera, South Australia. Launch vehicle based on Redstone. .

1967 November 29 - . 22:51 GMT - . Launch Site: Eglin. LV Family: Nike. Launch Vehicle: Nike Iroquois. LV Configuration: Nike Iroquois CRL AF07.658.
  • Smoke Aeronomy mission - . Nation: USA. Agency: AFCRL. Apogee: 121 km (75 mi).

1967 November 29 - . 22:51 GMT - . Launch Site: Eglin AFB. LV Family: Nike. Launch Vehicle: Nike Iroquois. LV Configuration: Nike Iroquois CRL AF07.661.
  • Smoke Aeronomy mission - . Nation: USA. Agency: AFCRL. Apogee: 122 km (75 mi).

1968 November 29 - .
  • No mention of results of planned December 1968 L1 launch in Kamanin's diary... - . Nation: USSR. Program: Lunar L1. Spacecraft: Soyuz 7K-L1. Summary: Kamanin states he will be travelling to the Far East for a reunion of his World War 2 unit. He will miss the state commission on the L1..

1968 November 29 - . 12:40 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC41/1. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 255 - . Payload: Zenit-2 11F61 s/n 68. Mass: 4,720 kg (10,400 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-2. Duration: 8.00 days. Decay Date: 1968-12-07 . USAF Sat Cat: 3574 . COSPAR: 1968-105A. Apogee: 317 km (196 mi). Perigee: 197 km (122 mi). Inclination: 65.4000 deg. Period: 89.60 min. Summary: Area survey photo reconnaissance satellite..

1968 November 29 - . 23:12 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA6A. LV Family: Europa. Launch Vehicle: Europa. LV Configuration: Europa I F-7. FAILURE: Third stage exploded.. Failed Stage: 3.
  • STV 1 / Europa F-7 - . Mass: 249 kg (548 lb). Nation: Europe. Agency: ELDO. Class: Technology. Type: Navigation technology satellite. Spacecraft: STV. Decay Date: 1968-11-30 . COSPAR: F681129A. Apogee: 230 km (140 mi). Summary: First attempt by ELDO to launch a satellite to orbit. Satellite Test Vehicle payload..

1969 November 29 - . 17:43 GMT - . Launch Site: South Uist. LV Family: Skua. Launch Vehicle: Skua 1.
  • Meteorological mission - . Nation: UK. Agency: MO-UK. Apogee: 60 km (37 mi).

1970 November 29 - . 15:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKMR. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 87 km (54 mi).

1971 November 29 - . 10:09 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC133/1. LV Family: Kosmos 2. Launch Vehicle: Kosmos 11K63.
  • Cosmos 458 - . Payload: DS-P1-Yu s/n 53. Mass: 325 kg (716 lb). Nation: USSR. Agency: MO. Program: DS. Class: Military. Type: Military target satellite. Spacecraft: DS-P1-Yu. Completed Operations Date: 1972-04-20 . Decay Date: 1972-04-20 . USAF Sat Cat: 5623 . COSPAR: 1971-101A. Apogee: 497 km (308 mi). Perigee: 271 km (168 mi). Inclination: 70.0000 deg. Period: 92.20 min. Summary: Development of systems for air defence and the control of outer space..

1971 November 29 - . 17:30 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 65027-110.
  • Cosmos 459 - . Payload: DS-P1-M s/n 5. Mass: 650 kg (1,430 lb). Nation: USSR. Agency: MO. Class: Military. Type: Anti-satellite system target. Spacecraft: DS-P1-M. Completed Operations Date: 1971-12-27 . Decay Date: 1971-12-27 . USAF Sat Cat: 5625 . COSPAR: 1971-102A. Apogee: 286 km (177 mi). Perigee: 199 km (123 mi). Inclination: 65.0000 deg. Period: 89.40 min. Summary: ASAT target for Cosmos 462 interceptor..

1972 November 29 - .
  • M2 Flight 40 - . Crew: Powell. Payload: M2-F3 flight 24. Nation: USA. Related Persons: Powell. Program: NASA Lifting Body. Class: Manned. Type: Manned spaceplane. Spacecraft: M2-F3. Summary: Maximum Speed - 1432 kph. Maximum Altitude - 20570 m. Flight Time - 357 sec..

1973 November 29 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-25 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1974 November 29 - . 10:17 GMT - . Launch Site: South Uist. LV Family: Petrel. Launch Vehicle: Petrel 1. LV Configuration: Petrel P182H.
  • Ionosphere mission - . Nation: UK. Agency: SRC. Apogee: 118 km (73 mi).

1974 November 29 - . 10:53 GMT - . Launch Site: South Uist. LV Family: Petrel. Launch Vehicle: Petrel 1. LV Configuration: Petrel P175H.
  • Atomic oxygen Atmospheric mission - . Nation: UK. Agency: SRC. Apogee: 134 km (83 mi).

1974 November 29 - . 12:09 GMT - . Launch Site: South Uist. LV Family: Petrel. Launch Vehicle: Petrel 1. LV Configuration: Petrel P179H.
  • Atomic oxygen Atmospheric mission - . Nation: UK. Agency: SRC. Apogee: 123 km (76 mi).

1975 November 29 - . 17:00 GMT - . Launch Site: Molodezhnaya. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 90 km (55 mi).

1976 November 29 - . 16:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 869 - . Payload: Soyuz 7K-S s/n 3L. Mass: 6,800 kg (14,900 lb). Nation: USSR. Agency: MOM. Program: Salyut 6. Class: Manned. Type: Manned spacecraft. Spacecraft: Soyuz 7K-S. Duration: 17.77 days. Decay Date: 1976-12-17 . USAF Sat Cat: 9564 . COSPAR: 1976-114A. Apogee: 289 km (179 mi). Perigee: 209 km (129 mi). Inclination: 51.7000 deg. Period: 89.40 min. Unmanned military Soyuz 7K-S test flight. Recovered December 17, 1976 10:31 GMT. Transmitted only on 20.008 MHz and 166 MHz frequencies, at none of the other usual Soyuz wavelengths.
    Maneuver Summary:
    196 km X 290 km orbit to 187 km X 335 km orbit. Delta V: 15 m/s
    187 km X 335 km orbit to 259 km X 335 km orbit. Delta V: 21 m/s
    259 km X 335 km orbit to 260 km X 345 km orbit. Delta V: 2 m/s
    260 km X 345 km orbit to 265 km X 368 km orbit. Delta V: 7 m/s
    265 km X 368 km orbit to 267 km X 391 km orbit. Delta V: 6 m/s
    267 km X 391 km orbit to 300 km X 310 km orbit. Delta V: 32 m/s
    Total Delta V: 83 m/s

1977 November 29 - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53721-265. FAILURE: Failure. Failed Stage: U.
  • Kosmos launch failure - . Nation: USSR. Agency: RVSN.

1977 November 29 - . Launch Site: Baikonur. Launch Complex: Baikonur LC109. LV Family: R-36M. Launch Vehicle: R-36M.
  • Missile accuracy test launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1978 November 29 - . 14:00 GMT - . Launch Site: Molodezhnaya. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 87 km (54 mi).

1979 November 29 - . 16:03 GMT - . Launch Site: Wallops Island. Launch Vehicle: Rocketsonde. LV Configuration: AN/DMQ-9.
  • - . Nation: USA. Agency: MRN. Apogee: 91 km (56 mi).

1982 November 29 - . 19:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: VOKV. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 83 km (51 mi).

1984 November 29 - . 14:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1613 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Earth. Type: Earth resources satellite. Spacecraft: Zenit-8. Duration: 25.00 days. Decay Date: 1984-12-24 . USAF Sat Cat: 15414 . COSPAR: 1984-121A. Apogee: 353 km (219 mi). Perigee: 194 km (120 mi). Inclination: 72.8000 deg. Period: 90.00 min. Summary: Military cartographic satellite; returned film capsule..

1985 November 29 - .
  • EVA STS-61-B-1 - . Crew: Ross; Spring. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.23 days. Nation: USA. Related Persons: Ross; Spring. Program: STS. Class: Manned. Type: Manned spaceplane. Flight: STS-61-B. Spacecraft: Atlantis. Summary: Began EASE/ACCESS (Assembly of Structures / Assembly Concept for Construction of Erectable Space Structures) structural assembly experiments..

1986 November 29 - . 08:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/40. LV Family: Proton. Launch Vehicle: Proton-K. LV Configuration: Proton-K 338-01. FAILURE: Second stage explosion.. Failed Stage: 2.
  • Almaz-T s/n 303 Failure - . Payload: Almaz-K s/n 303. Mass: 18,550 kg (40,890 lb). Nation: USSR. Agency: UNKS. Program: Almaz. Class: Surveillance. Type: Civilian surveillance radar satellite. Spacecraft: Almaz-T. Decay Date: 1986-12-29 . COSPAR: F861129A. Summary: In the second half of 1986 the first Almaz-T s/n 303 was readied for launch. General V V Favorskiy ordered it to be completed and launched with a full-up lab module in place of trials equipment. Unfortunately did not reach orbit..

1987 November 29 - . 03:28 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Titan. Launch Vehicle: Titan 34D/Transtage. LV Configuration: Titan 34D/Transtage 34D-8 (05D-4).
  • USA 28 - . Payload: DSP Phase 2 Upgrade s/n 5R. Mass: 1,670 kg (3,680 lb). Nation: USA. Agency: USAF. Class: Military. Type: Early warning satellite. Spacecraft: DSP. Completed Operations Date: 1987-12-31 . USAF Sat Cat: 18583 . COSPAR: 1987-097A. Apogee: 35,558 km (22,094 mi). Perigee: 35,514 km (22,067 mi). Inclination: 2.9000 deg. Period: 1,423.30 min. Reserve DSP ballistic missile launch detection satellite fitted with Block 14 sensors, remained in service for only five years.. Observed Scud launches during Gulf War. Positioned in geosynchronous orbit at 35 deg W in 1988-1989; 10 deg E in 1989-1992; 35 deg W in 1992-1993; 105 deg E in 1993; 165 deg W in 1999.

1988 November 29 - . 22:18 GMT - . Launch Site: Kwajalein. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 69 km (42 mi).

1989 November 29 - . 14:07 GMT - . Launch Site: Molodezhnaya. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 82 km (50 mi).

1990 November 29 - . 11:30 GMT - . Launch Site: Sea-launched. Launch Pad: SAIN. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 83 km (51 mi).

1993 November 29 - . 09:30 GMT - . Launch Site: Kiruna. LV Family: Hawk. Launch Vehicle: Nike Orion Improved. LV Configuration: Nike Improved Orion DLR K-NO2-206.
  • Mini-Texus 1 Microgravity mission - . Nation: Germany. Agency: DLR. Apogee: 146 km (90 mi).

1994 November 29 - . 02:54 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32/2. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Geo-IK - . Payload: Geo-IK no. 14. Mass: 1,500 kg (3,300 lb). Nation: Russia. Agency: RAKA. Class: Earth. Type: Geodetic satellite. Spacecraft: Geo-IK. USAF Sat Cat: 23411 . COSPAR: 1994-078A. Apogee: 1,526 km (948 mi). Perigee: 1,481 km (920 mi). Inclination: 73.6000 deg. Period: 116.10 min. Summary: Also tested Elekon communcations payload..

1994 November 29 - . 10:21 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36A. LV Family: Atlas. Launch Vehicle: Atlas IIA. LV Configuration: Atlas IIA AC-110 / Centaur II 8109.
  • Orion 1 - . Mass: 2,358 kg (5,198 lb). Nation: USA. Agency: Orion. Manufacturer: Toulouse. Program: Orion. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 2000. USAF Sat Cat: 23413 . COSPAR: 1994-079A. Apogee: 35,792 km (22,240 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.0000 deg. Period: 1,436.10 min. 34 Ku-band transponders for TV. Stationed at 37.48 deg W. Launch vehicle put payload into supersynchronous earth orbit with IFR trajectory option. Positioned in geosynchronous orbit at 37 deg W in 1994-1999 As of 5 September 2001 located at 37.54 deg W drifting at 0.010 deg W per day. As of 2007 Mar 11 located at 37.60W drifting at 0.015W degrees per day.

1994 November 29 - . 17:02 GMT - . Launch Site: Xichang. Launch Complex: Xichang LC2. LV Family: CZ. Launch Vehicle: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-2 (36).
  • Zhongxing-5 - . Mass: 2,230 kg (4,910 lb). Nation: China. Agency: Chinasat. Program: Chinasat. Class: Communications. Type: Military communications satellite. Spacecraft: DFH-3. Completed Operations Date: 1994-12-01 . USAF Sat Cat: 23415 . COSPAR: 1994-080A. Apogee: 35,957 km (22,342 mi). Perigee: 35,225 km (21,887 mi). Inclination: 0.1500 deg. Period: 1,426.15 min. The first test launch of a DFH-3 by a CZ-3A launch vehicle was successful in attaining the proper transfer orbit, but during the subsequent manoeuvres to achieve geostationary orbit, the DFH-3 failed due to a malfunction of the satellite on-board propulsion system. The satellite was positioned at 132 deg E prior to the failure. As of 4 September 2001 located at 113.80 deg E drifting at 2.499 deg E per day. As of 2007 Mar 2 located at 90.02E drifting at 2.513E degrees per day.

1995 November 29 - . 02:05 GMT - . Launch Site: Ryori. LV Family: MT-135. Launch Vehicle: MT-135P. LV Configuration: MT-135P-R945.
  • Meteorological mission - . Nation: Japan. Agency: JMA. Apogee: 60 km (37 mi).

1996 November 29 - . Launch Site: Plesetsk. LV Family: RT-23. Launch Vehicle: RT-23U 15Zh61. LV Configuration: RT-23U 15Zh61 15Zh61.
  • rail - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

2000 November 29 - .
  • Discovery of Y000593 Meteorite (Mars Meteorite) - . Nation: Japan.

2002 November 29 - . 18:36 GMT - .
  • EVA STS-113-2 - . Crew: Lopez-Alegria; Herrington. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.26 days. Nation: USA. Related Persons: Lopez-Alegria; Herrington. Program: ISS. Flight: STS-113. Summary: The astronauts emerged from the Quest module at about 1845 UTC. They removed P1 keel pins and installed TV cameras, and moved the CETA-2 cart from P1 to S1..

2003 November 29 - . 04:33 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-IIA 2024. LV Configuration: H-IIA 2024 H-IIA-6F. FAILURE: Destroyed by range safety after solid booster nozzle burn-through resulted in motor not separating from core.. Failed Stage: 0.
  • IGS-2a - . Mass: 850 kg (1,870 lb). Nation: Japan. Agency: NASDA. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: IGS. COSPAR: F20031129A. Summary: The launch failure meant that Japan's planned intelligence satellite constellation was crippled. The system was already in trouble due to the reported poor performance of the first two elements launched..
  • IGS-2b - . Mass: 1,200 kg (2,600 lb). Nation: Japan. Agency: NASDA. Class: Surveillance. Type: Civilian surveillance radar satellite. Spacecraft: IGS. COSPAR: F20031129B.

2004 November 29 - .
  • Soyuz TMA-5 moved - . Nation: Russia. Related Persons: Chiao; Sharipov. Program: ISS. Flight: ISS EO-10. The EO-10 crew entered Soyuz TMA-5, undocked it from the Pirs module of the International Space Station at 09:32 GMT and redocked it at the nearby Zarya module at 09:53 GMT. This cleared the Pirs docking port for the expected arrival of a Progress unmanned logistics spacecraft.

2005 November 29 - . 07:44 GMT - . Launch Site: Plesetsk. LV Family: Topol. Launch Vehicle: Topol. LV Configuration: Topol 81.
  • PBS test 1 - . Nation: Russia. Agency: RVSN. Apogee: 1,000 km (600 mi).

2006 November 29 - . Launch Site: Sonmiani. LV Family: DF-15. Launch Vehicle: Shaheen 1. LV Configuration: Shaheen 1 Haft-4.
  • - . Nation: Pakistan. Apogee: 100 km (60 mi).

2007 November 29 - .
  • ISS On-Orbit Status 11/29/07 - . Nation: USA. Related Persons: Love; Malenchenko; Tani; Whitson. Program: ISS. Flight: ISS EO-16; STS-122. Upon wakeup, FE-1 Malenchenko terminated his third MBI-12 SONOKARD experiment session by taking the recording device from his SONOKARD sports shirt pocket and later copying the measurements to the RSE-MED laptop for subsequent downlink to the ground.

    (SONOKARD objectives are stated to (1) study the feasibility of obtaining the maximum of data through computer processing of records obtained overnight, (2) systematically record the crewmember's physiological functions during sleep, (3) study the feasibility of obtaining real-time crew health data. Investigators believe that contactless acquisition of cardiorespiratory data over the night period could serve as a basis for developing efficient criteria for evaluating and predicting adaptive capability of human body in long-duration space flight.) Additional Details: ISS On-Orbit Status 11/29/07.


2009 November 29 - . 09:00 GMT - . Launch Site: Kiruna. LV Family: Sonda. Launch Vehicle: VSB-30.
  • TEXUS 47 - . Nation: Sweden. Summary: Microgravity experiments.

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